CN112848967B - Unmanned aerial vehicle battery management system capable of improving comprehensive utilization rate - Google Patents
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L58/00—Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles
- B60L58/10—Methods or circuit arrangements for monitoring or controlling batteries or fuel cells, specially adapted for electric vehicles for monitoring or controlling batteries
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The invention discloses an unmanned aerial vehicle battery management system capable of improving the comprehensive utilization rate, which comprises a battery electric quantity calculation module, an unmanned aerial vehicle power calculation module, a control processing module and a transmission receiving module, wherein the battery electric quantity calculation module comprises a battery voltage stabilization transmission module, a battery voltage and current measurement module and a residual electric quantity estimation module, and the unmanned aerial vehicle power calculation module comprises an unmanned aerial vehicle working condition analysis module and an operation power real-time measurement module. And controlling the unmanned aerial vehicle.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle battery management system capable of improving the comprehensive utilization rate.
Background
Unmanned aerial vehicle, unmanned aerial vehicle for short, utilize radio remote control equipment and self-contained program control device to control the unmanned aerial vehicle, unmanned aerial vehicle is the general name of unmanned aerial vehicle in fact, unmanned aerial vehicle according to the application field, can be divided into military use and civilian use, the military use aspect, unmanned aerial vehicle is divided into reconnaissance plane and target plane, the civilian use, the application of unmanned aerial vehicle trade, it is the real just-in-need of unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the use of the unmanned aerial vehicle is greatly expanded, and the existing unmanned aerial vehicle generally uses a battery to provide a power supply when in operation;
the unmanned aerial vehicle battery management system who has now on the existing market is when implementing, and the unmanned aerial vehicle battery is when moving, because of unmanned aerial vehicle power change easily, leads to the continuation of the journey of unmanned aerial vehicle battery to show and the deviation appears, and the unmanned aerial vehicle battery is after using for a long time, voltage and current instability when appearing battery output electric quantity easily influence unmanned aerial vehicle's use.
Disclosure of Invention
The technical scheme provided by the invention can effectively solve the problems that the endurance display of the unmanned aerial vehicle battery is easy to deviate due to the power change of the unmanned aerial vehicle when the unmanned aerial vehicle battery provided by the background technology operates, and the voltage and the current of the battery output electricity are easy to be unstable after the unmanned aerial vehicle battery is used for a long time, so that the use of the unmanned aerial vehicle is influenced.
In order to achieve the purpose, the invention provides the following technical scheme: an unmanned aerial vehicle battery management system capable of improving comprehensive utilization rate comprises a battery power calculation module, an unmanned aerial vehicle power calculation module, a control processing module and a transmission receiving module, wherein the battery power calculation module comprises a battery voltage stabilization transmission module, a battery voltage and current measurement module and a residual power estimation module;
the output of battery power calculation module is connected with unmanned aerial vehicle power calculation module's input, the input of battery power calculation module is connected with control processing module's output, control processing module's input is connected with transmission receiving module's output.
According to the technical characteristics, the battery power calculation module comprises a battery voltage stabilization transmission module, a battery voltage and current measurement module and a residual power estimation module, wherein the battery voltage stabilization transmission module comprises a voltage stabilizer and a current stabilization electrolytic capacitor, the battery voltage and current measurement module comprises current measurement and voltage measurement, and the residual power estimation module comprises battery discharge capacity measurement and battery residual power calculation.
According to the technical characteristics, the battery voltage-stabilizing transmission module comprises a voltage stabilizer and a current-stabilizing electrolytic capacitor, wherein the voltage stabilizer is used for reducing the fluctuation of the output voltage of the battery and keeping the voltage stability when the parallel battery outputs the electric quantity, and the current-stabilizing electrolytic capacitor is used for reducing the fluctuation of the output current of the battery and improving the current stability when the parallel battery outputs the electric quantity;
the battery voltage and current measuring and calculating module comprises current measuring and calculating and voltage measuring and calculating, wherein the current measuring and calculating refers to measuring and calculating a stable current value when the battery outputs electricity, and the voltage measuring and calculating refers to measuring and calculating a stable battery voltage value when the battery outputs electricity.
According to the technical characteristics, the residual electric quantity estimation module comprises battery discharge quantity metering and battery residual electric quantity calculation, wherein the battery discharge quantity metering refers to metering single discharge quantity and total discharge quantity of each unmanned aerial vehicle battery, and transmitting the metered data, and the battery residual electric quantity calculation refers to calculating residual electric quantity of each unmanned aerial vehicle battery, and transmitting the calculated data.
According to the technical characteristics, the unmanned aerial vehicle power calculation module comprises an unmanned aerial vehicle working condition analysis module and an operation power real-time measurement and calculation module, the unmanned aerial vehicle working condition analysis module comprises electric element power supply monitoring and unmanned aerial vehicle flight working condition analysis, and the operation power real-time measurement and calculation module comprises electric element operation monitoring and electric element power calculation.
According to the technical characteristics, the unmanned aerial vehicle working condition analysis module comprises electric element power supply monitoring and unmanned aerial vehicle flight working condition analysis, wherein the electric element power supply monitoring refers to self-detection of the power supply condition of an electric element in the unmanned aerial vehicle, and meanwhile, real-time monitoring of the running state of the electric element is carried out, and the unmanned aerial vehicle flight working condition analysis refers to monitoring and analysis of specific conditions of each component of the unmanned aerial vehicle and real-time transmission of analyzed data;
the real-time operating power measuring and calculating module comprises electric element operation monitoring and electric element power calculation, wherein the electric element operation monitoring refers to the real-time monitoring of the operation condition of the power supply electric element, the real-time transmission of the actual power data of the electric element is carried out according to the operation condition of the electric element, and the electric element power calculation refers to the real-time receiving of the actual power data of each electric element, and the real-time total power of the electric element during the flight of the unmanned aerial vehicle is calculated.
According to the technical characteristics, the control processing module comprises an unmanned aerial vehicle control module, an unmanned aerial vehicle information processing module and a remote control module, the unmanned aerial vehicle control module comprises an unmanned aerial vehicle controller, the unmanned aerial vehicle information processing module comprises an unmanned aerial vehicle processor and an unmanned aerial vehicle information memory, and the remote control module comprises an unmanned aerial vehicle remote control terminal.
According to the technical characteristics, the unmanned aerial vehicle control module comprises an unmanned aerial vehicle controller, and the unmanned aerial vehicle controller is used for receiving the control instruction transmitted remotely and controlling the corresponding electrical components to operate according to the received control instruction;
the unmanned aerial vehicle information processing module comprises an unmanned aerial vehicle processor and an unmanned aerial vehicle information memory, the unmanned aerial vehicle processor is used for receiving measured battery voltage and current value data, battery single discharge data, battery residual current data and real-time total power data of electrical components of the unmanned aerial vehicle during flying, performing processing operation and calculating the estimated endurance time and endurance mileage of the unmanned aerial vehicle under the condition of specified power, and the unmanned aerial vehicle information memory is used for locally storing the data monitored by the unmanned aerial vehicle and the calculated data;
the remote control module comprises an unmanned aerial vehicle remote control terminal, and the unmanned aerial vehicle remote control terminal is a terminal controller for remotely controlling the unmanned aerial vehicle by a user.
According to the above technical features, the transmission and reception module includes a radio transmission module and a GPRS signal transmission module, the radio transmission module includes an unmanned aerial vehicle radio transmission and a remote control terminal radio transmission.
According to the technical characteristics, the radio transmission module comprises unmanned aerial vehicle radio transmission and remote control terminal radio transmission, the unmanned aerial vehicle radio transmission refers to radio transmission of a control instruction transmitted by the remote control terminal in a radio signal receiving range, and the remote control terminal radio transmission refers to radio reception of the control instruction transmitted by the remote control terminal in the radio signal receiving range;
GPRS signal transmission module includes unmanned aerial vehicle GPRS transmission and remote control terminal radio transmission, unmanned aerial vehicle GPRS transmission is in order to transmit the control command of remote control terminal transmission through the GPRS network under the unable circumstances of receiving of radio, remote control terminal radio transmission is in order to receive through the GPRS network under the unable circumstances of receiving of radio, unmanned aerial vehicle to the control command of remote control terminal transmission.
Compared with the prior art, the invention has the following beneficial effects: the invention has scientific and reasonable structure and safe and convenient use:
1. through stabiliser and stationary flow electrolytic capacitor in the battery steady voltage transmission module, can reduce battery output voltage and output current's fluctuation, voltage stability and current stability when keeping parallelly connected battery output power, through carry out measurement calculation to the steady current value when battery output power and battery voltage value, measure the single discharge capacity and the total discharge capacity of every unmanned aerial vehicle battery again, can carry out the analysis and calculation to the residual capacity of every unmanned aerial vehicle battery, thereby keep the stability of unmanned aerial vehicle battery power transmission, reduce unmanned aerial vehicle battery power transmission unstability, influence the utilization ratio of electric quantity in the unmanned aerial vehicle battery, can improve the comprehensive utilization ratio of unmanned aerial vehicle electric quantity from basic, also reduce the damage that unmanned aerial vehicle power output unstability produced electric elements.
2. The power supply condition of electrical components in the unmanned aerial vehicle is automatically detected, the running state of the electrical components is monitored in real time, the specific conditions of each component of the unmanned aerial vehicle are monitored and analyzed, the damaged components of the unmanned aerial vehicle can be monitored in time, the running condition of the electrical components for supplying power is monitored in real time, the real-time total power of the electrical components of the unmanned aerial vehicle during flying is calculated by measurement, then the estimated endurance time and endurance mileage of the unmanned aerial vehicle under the condition of specified power can be calculated according to the measured battery voltage and current value data, the battery single discharge data, the battery residual current data and the real-time total power data of the electrical components of the unmanned aerial vehicle during flying, so that the power of each component of the unmanned aerial vehicle and the total power of the whole unmanned aerial vehicle can be accurately calculated, and a user can conveniently and accurately calculate the endurance time and the estimated endurance mileage of the unmanned aerial vehicle according to the real-time power and the estimated endurance mileage of the unmanned aerial vehicle, and controlling the unmanned aerial vehicle.
3. The endurance time and the endurance mileage are transmitted to the unmanned aerial vehicle remote control terminal in a radio and GPRS signal mode, the unmanned aerial vehicle remote control terminal is presented to a user, corresponding control instructions can be transmitted according to the received endurance time and the received endurance mileage, the control instructions are transmitted to the unmanned aerial vehicle in a radio and GPRS signal transmission mode, the control instructions are received by an unmanned aerial vehicle controller in the unmanned aerial vehicle, corresponding electrical elements are controlled to run, unnecessary electrical elements can be reduced to run, unnecessary loss of electric quantity of an unmanned aerial vehicle battery is reduced, the unmanned aerial vehicle can be remotely controlled to run, and the situation that signal transmission is weak due to the fact that the distance is too far and the unmanned aerial vehicle is remotely controlled can be avoided.
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The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention.
In the drawings:
FIG. 1 is a schematic diagram of the system architecture of the present invention.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it should be understood that they are presented herein only to illustrate and explain the present invention and not to limit the present invention.
Example (b): as shown in fig. 1, the present invention provides a technical solution, an unmanned aerial vehicle battery management system capable of improving comprehensive utilization rate, comprising a battery power calculation module, an unmanned aerial vehicle power calculation module, a control processing module and a transmission and reception module, wherein the battery power calculation module comprises a battery voltage stabilization transmission module, a battery voltage and current measurement module and a residual power estimation module, the unmanned aerial vehicle power calculation module comprises an unmanned aerial vehicle working condition analysis module and an operation power real-time measurement and calculation module, the control processing module comprises an unmanned aerial vehicle control module, an unmanned aerial vehicle information processing module and a remote control module, and the transmission and reception module comprises a radio transmission module and a GPRS signal transmission module;
the output end of the battery electric quantity calculation module is connected with the input end of the unmanned aerial vehicle power calculation module, the input end of the battery electric quantity calculation module is connected with the output end of the control processing module, and the input end of the control processing module is connected with the output end of the transmission and reception module.
According to the technical characteristics, the battery power calculation module comprises a battery voltage-stabilizing transmission module, a battery voltage and current measurement module and a residual power estimation module, the battery voltage-stabilizing transmission module comprises a voltage stabilizer and a current-stabilizing electrolytic capacitor, the battery voltage and current measurement module comprises current measurement and voltage measurement, and the residual power estimation module comprises battery discharge capacity measurement and battery residual power calculation.
According to the technical characteristics, the battery voltage-stabilizing transmission module comprises a voltage stabilizer and a current-stabilizing electrolytic capacitor, wherein the voltage stabilizer is used for reducing the fluctuation of the output voltage of the battery and keeping the voltage stability when the parallel battery outputs the electric quantity, and the current-stabilizing electrolytic capacitor is used for reducing the fluctuation of the output current of the battery and improving the current stability when the parallel battery outputs the electric quantity;
the battery voltage and current measuring and calculating module comprises current measuring and calculating and voltage measuring and calculating, wherein the current measuring and calculating refers to measuring and calculating a stable current value when the battery outputs electric quantity, and the voltage measuring and calculating refers to measuring and calculating a stable battery voltage value when the battery outputs electric quantity.
According to the technical characteristics, the residual electric quantity estimation module comprises battery discharge quantity metering and battery residual electric quantity calculation, wherein the battery discharge quantity metering refers to metering single discharge quantity and total discharge quantity of each unmanned aerial vehicle battery and transmitting the metered data, and the battery residual electric quantity calculation refers to calculating residual electric quantity of each unmanned aerial vehicle battery and transmitting the calculated data.
According to the technical characteristics, the unmanned aerial vehicle power calculation module comprises an unmanned aerial vehicle working condition analysis module and an operation power real-time measurement and calculation module, the unmanned aerial vehicle working condition analysis module comprises electric element power supply monitoring and unmanned aerial vehicle flight working condition analysis, and the operation power real-time measurement and calculation module comprises electric element operation monitoring and electric element power calculation.
According to the technical characteristics, the unmanned aerial vehicle working condition analysis module comprises electric element power supply monitoring and unmanned aerial vehicle flight working condition analysis, wherein the electric element power supply monitoring refers to the self-detection of the power supply condition of an electric element in the unmanned aerial vehicle, the real-time monitoring of the running state of the electric element is carried out at the same time, and the unmanned aerial vehicle flight working condition analysis refers to the monitoring and analysis of the specific conditions of each component of the unmanned aerial vehicle and the real-time transmission of the analyzed data;
the real-time operating power measuring and calculating module comprises electric element operation monitoring and electric element power calculation, the electric element operation monitoring means real-time monitoring of the operation condition of the power supply electric element and real-time transmission of actual power data of the electric element according to the operation condition of the electric element, and the electric element power calculation means real-time receiving of the actual power data of each electric element and calculation of the real-time total power of the electric element during flight of the unmanned aerial vehicle.
According to above-mentioned technical characteristics, control processing module includes unmanned aerial vehicle control module, unmanned aerial vehicle information processing module and remote control module, and unmanned aerial vehicle control module includes the unmanned aerial vehicle controller, and unmanned aerial vehicle information processing module includes unmanned aerial vehicle treater and unmanned aerial vehicle information storage ware, and remote control module includes unmanned aerial vehicle remote control terminal.
According to the technical characteristics, the unmanned aerial vehicle control module comprises an unmanned aerial vehicle controller, and the unmanned aerial vehicle controller is used for receiving the control instruction transmitted remotely and controlling the corresponding electrical components to operate according to the received control instruction;
the unmanned aerial vehicle information processing module comprises an unmanned aerial vehicle processor and an unmanned aerial vehicle information memory, the unmanned aerial vehicle processor is used for receiving measured battery voltage and current value data, battery single discharge data, battery residual current data and real-time total power data of electrical components of the unmanned aerial vehicle during flying, processing and operating the data and calculating the estimated endurance time and endurance mileage of the unmanned aerial vehicle under the condition of specified power, and the unmanned aerial vehicle information memory is used for locally storing the data monitored by the unmanned aerial vehicle and the calculated data;
the remote control module comprises an unmanned aerial vehicle remote control terminal, and the unmanned aerial vehicle remote control terminal is a terminal controller for remotely controlling the unmanned aerial vehicle by a user.
According to the technical characteristics, the transmission and receiving module comprises a radio transmission module and a GPRS signal transmission module, and the radio transmission module comprises unmanned aerial vehicle radio transmission and remote control terminal radio transmission.
According to the technical characteristics, the radio transmission module comprises unmanned aerial vehicle radio transmission and remote control terminal radio transmission, the unmanned aerial vehicle radio transmission refers to carrying out radio transmission on the control instruction transmitted by the remote control terminal in a radio signal receiving range, and the remote control terminal radio transmission refers to carrying out radio reception on the control instruction transmitted by the remote control terminal in the radio signal receiving range;
the GPRS signal transmission module comprises unmanned aerial vehicle GPRS transmission and remote control terminal radio transmission, the unmanned aerial vehicle GPRS transmission is used for transmitting a control instruction transmitted by a remote control terminal through a GPRS network under the condition that radio cannot be received, and the remote control terminal radio transmission is used for receiving the control instruction transmitted by the remote control terminal through the GPRS network under the condition that the radio cannot be received by the unmanned aerial vehicle.
The working principle and the using process of the invention are as follows: when the unmanned aerial vehicle battery management system capable of improving the comprehensive utilization rate operates, the electric quantity in the unmanned aerial vehicle battery is transmitted out when the unmanned aerial vehicle operates, the fluctuation of the output voltage and the output current of the battery can be reduced through a voltage stabilizer and a current stabilizing electrolytic capacitor in a battery voltage stabilizing transmission module, the voltage stability and the current stability when the batteries connected in parallel output the electric quantity are kept, the stable current value and the battery voltage value when the batteries output the electric quantity can be measured and calculated, and then the single discharge quantity and the total discharge quantity of each unmanned aerial vehicle battery are measured, so that the residual electric quantity of each unmanned aerial vehicle battery is analyzed and calculated, the electric quantity transmission stability of the unmanned aerial vehicle battery can be kept, the unstable electric quantity transmission of the unmanned aerial vehicle battery is reduced, and the utilization rate of the electric quantity in the unmanned aerial vehicle battery is influenced;
meanwhile, the power supply condition of electrical components in the unmanned aerial vehicle is automatically detected, and the running state of the electrical components is monitored in real time, the specific conditions of each component of the unmanned aerial vehicle are monitored and analyzed, the damaged components of the unmanned aerial vehicle are monitored in time, the operation condition of the power supply electrical appliance element is monitored in real time, and transmits the actual power data of the electrical components according to the operating conditions of the electrical components, calculating the real-time total power of electrical components when the unmanned aerial vehicle flies by using the unmanned aerial vehicle processor, and then calculating the predicted endurance time and endurance mileage of the unmanned aerial vehicle under the condition of specified power according to the measured battery voltage and current value data, battery single discharge data, battery residual current data and the real-time total power data of the electrical components when the unmanned aerial vehicle flies, so that the power of each component of the unmanned aerial vehicle and the total power of the whole unmanned aerial vehicle can be accurately calculated;
the mode through radio and GPRS signal is with duration and duration mileage transmission to unmanned aerial vehicle remote control terminal afterwards, thereby present the user through the display at unmanned aerial vehicle remote control terminal, the user can be according to the duration and the duration mileage of receipt, transmit corresponding control command, mode through radio and GPRS signal transmission, transmit control command to unmanned aerial vehicle, receive control command by unmanned aerial vehicle controller in the unmanned aerial vehicle, control corresponding electrical components operation, can reduce unnecessary electrical components operation, thereby reduce the unnecessary loss of unmanned aerial vehicle battery electric quantity.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle battery management system capable of improving comprehensive utilization rate is characterized by comprising a battery power calculation module, an unmanned aerial vehicle power calculation module, a control processing module and a transmission and reception module, wherein the battery power calculation module comprises a battery voltage stabilization transmission module, a battery voltage and current measurement module and a residual power estimation module;
the output end of the battery electric quantity calculation module is connected with the input end of the unmanned aerial vehicle power calculation module, the input end of the battery electric quantity calculation module is connected with the output end of the control processing module, and the input end of the control processing module is connected with the output end of the transmission and reception module;
the unmanned aerial vehicle power calculation module comprises an unmanned aerial vehicle working condition analysis module and an operation power real-time measurement and calculation module, the unmanned aerial vehicle working condition analysis module comprises electric appliance element power supply monitoring and unmanned aerial vehicle flight working condition analysis, and the operation power real-time measurement and calculation module comprises electric appliance element operation monitoring and electric appliance element power calculation;
the unmanned aerial vehicle working condition analysis module comprises electric element power supply monitoring and unmanned aerial vehicle flight working condition analysis, wherein the electric element power supply monitoring refers to self-detection of the power supply condition of an electric element in the unmanned aerial vehicle, and real-time monitoring of the operation state of the electric element, and the unmanned aerial vehicle flight working condition analysis refers to monitoring and analysis of specific conditions of each component of the unmanned aerial vehicle and real-time transmission of analyzed data;
the real-time operating power measuring and calculating module comprises electric element operating monitoring and electric element power calculation, wherein the electric element operating monitoring refers to the real-time monitoring of the operating condition of a power-supplied electric element and the real-time transmission of the actual power data of the electric element according to the operating condition of the electric element, and the electric element power calculation refers to the real-time receiving of the actual power data of each electric element and the calculation of the real-time total power of the electric element during the flight of the unmanned aerial vehicle;
the control processing module comprises an unmanned aerial vehicle control module, an unmanned aerial vehicle information processing module and a remote control module, the unmanned aerial vehicle control module comprises an unmanned aerial vehicle controller, the unmanned aerial vehicle information processing module comprises an unmanned aerial vehicle processor and an unmanned aerial vehicle information memory, and the remote control module comprises an unmanned aerial vehicle remote control terminal;
the unmanned aerial vehicle control module comprises an unmanned aerial vehicle controller, and the unmanned aerial vehicle controller is used for receiving a control instruction transmitted remotely and controlling corresponding electrical components to operate according to the received control instruction;
the unmanned aerial vehicle information processing module comprises an unmanned aerial vehicle processor and an unmanned aerial vehicle information memory, wherein the unmanned aerial vehicle processor is used for receiving measured battery voltage and current value data, battery single discharge data, battery residual current data and real-time total power data of electrical components of the unmanned aerial vehicle during flying, performing processing operation and calculating the estimated endurance time and endurance mileage of the unmanned aerial vehicle under the condition of specified power, and the unmanned aerial vehicle information memory is used for locally storing the data monitored by the unmanned aerial vehicle and the calculated data;
the remote control module comprises an unmanned aerial vehicle remote control terminal, and the unmanned aerial vehicle remote control terminal is a terminal controller for remotely controlling the unmanned aerial vehicle by a user.
2. The UAV battery management system according to claim 1, wherein the battery power calculating module comprises a battery voltage stabilizing transmission module, a battery voltage and current measuring module and a remaining power estimating module, the battery voltage stabilizing transmission module comprises a voltage stabilizer and a current stabilizing electrolytic capacitor, the battery voltage and current measuring module comprises a current measuring and a voltage measuring, and the remaining power estimating module comprises a battery discharge capacity measuring and a battery remaining power calculating.
3. The unmanned aerial vehicle battery management system capable of improving the comprehensive utilization rate of the battery of claim 2, wherein the battery voltage stabilizing transmission module comprises a voltage stabilizer and a current stabilizing electrolytic capacitor, the voltage stabilizer is used for reducing the fluctuation of the output voltage of the battery and maintaining the voltage stability when the parallel battery outputs the electric quantity, and the current stabilizing electrolytic capacitor is used for reducing the fluctuation of the output current of the battery and improving the current stability when the parallel battery outputs the electric quantity;
the battery voltage and current measuring and calculating module comprises current measuring and calculating and voltage measuring and calculating, wherein the current measuring and calculating refers to measuring and calculating a stable current value when the battery outputs electric quantity, and the voltage measuring and calculating refers to measuring and calculating a stable battery voltage value when the battery outputs electric quantity.
4. The unmanned aerial vehicle battery management system capable of improving the comprehensive utilization rate of the power supply according to claim 2, wherein the remaining power estimation module comprises battery discharge capacity metering and battery remaining power calculation, the battery discharge capacity metering refers to metering of single discharge capacity and total discharge capacity of each unmanned aerial vehicle battery, and transmission of the metered data, and the battery remaining power calculation refers to calculation of remaining power of each unmanned aerial vehicle battery, and transmission of the calculated data.
5. The system according to claim 1, wherein the transmission and reception module comprises a radio transmission module and a GPRS signal transmission module, and the radio transmission module comprises a drone radio transmission and a remote control terminal radio transmission.
6. The battery management system for unmanned aerial vehicles capable of improving comprehensive utilization rate of the battery according to claim 5, wherein the radio transmission module comprises an unmanned aerial vehicle radio transmission and a remote control terminal radio transmission, the unmanned aerial vehicle radio transmission is used for performing radio transmission on the control command transmitted by the remote control terminal in a radio signal receiving range, and the remote control terminal radio transmission is used for performing radio reception on the control command transmitted by the remote control terminal in the radio signal receiving range;
GPRS signal transmission module includes unmanned aerial vehicle GPRS transmission and remote control terminal radio transmission, unmanned aerial vehicle GPRS transmission is in order to transmit the control command of remote control terminal transmission through the GPRS network under the unable circumstances of receiving of radio, remote control terminal radio transmission is in order to receive through the GPRS network under the unable circumstances of receiving of radio, unmanned aerial vehicle to the control command of remote control terminal transmission.
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